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Designing WIG Airfoil
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M_Nirooei@alum.sharif.edu
. () . 1
. .
. ) 3(2
.
.
. 0.2 2738309.8 . NACA 4412
. 2 .
IGE//Name
-0.100382.890.00850.7066NACA 4412-0.062577.540.00860.6699New Airfoil
OGE-0.093563.760.01020.6532NACA 4412-0.053358.450.01010.5926New Airfoil
1 Center of height2 De-cambering3 Reflex
%6.45) IGE (/
%37.68
. )OGE( .
. . %43/ 8.32%/
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